FLIGHT MANAGEMENT SYSTEM REQUIREMENT ANALYSIS FOR TRAJECTORY BASED OPERATION
Hovering Formation Design and Control Based on Relative Orbit Elements (AAS 14-377)
Design of Lunar Free-Return Trajectories Based on UKF Parameter Estimation (AAS 14-469)
Collision Avoidance in Elliptical Formation Flying Based on Relative Orbit Elements (AAS 14-208)
Space-Time Coordinate Systems in the High-Precision Orbit Prediction (AAS 14-291)
Optimal Low-Thrust Transfer and Guidance Scheme for Geostationary Orbit Insertion (AAS 14-386)
Reliability Analysis of SGP4 Using GOCE Satellite (AIAA 2014-4281)
Indirect Optimization of Low-Thrust Earth Escape Trajectories (AAS 13-305)
Study of Elliptical Relative Motion Control Based on Relative Orbit Elements (AAS 13-474)